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ForceTally · AI-generated illustration · Not a photograph · AI-generated · OpenAI output terms · Source ↗ · Modified
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At a glance
Nagastra-1larger figure on 1 of 1
WB Electronics Warmatelarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | Nagastra-1 | WB Electronics Warmate |
|---|---|---|
| Type | Unmanned aerial vehicle Loitering munition[source] | Loitering munition[source] |
| Place of origin | India[source] | Poland[source] |
| Used by | Indian Army[source] | See Operators[source] |
| Wars | 2025 India–Pakistan conflict[source] | Russian invasion of Ukraine 2025 India–Pakistan strikes |
Width
Single source1.6 m (5 ft 3 in)[source]
Mass
Single source8–9 kg (18–20 lb)[source]
Empty
Single sourceEmpty; Empty weight
Single sourceMaximum take-off; Maximum take-off weight
Single sourceMTOW Warmate
Single sourceWarmate 2
Single sourceWeight
DisputedEmpty: 4 kg (8.8 lb) MTOW : 5.7 kg (13 lb) (Warmate), 30 kg (66 lb) (Warmate 2)[source]
4 kilograms (8.8 lb)[source]
5.2 kilograms (11 lb)[source]
5.7 kilograms (12.6 lb)[source]
5.7 kg[source]
5.7 kg[source]
5.7 kg[source]
Operational; Operational range
Single source30–40 km (19–25 mi)[source]
Warmate; base-model specification subsection
Single source1.4 kilograms (3.1 lb)[source]Warmate; base-model specification subsection
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Z-Motion Autonomous Systems Economic Explosives Limited[source] | — |
|---|
| Manufacturer | Economic Explosives Limited[source] | WB Electronics[source] |
|---|
| Produced | 2024–current[source] | 2016–current[source] |
|---|
| Warhead | High-explosive fragmentation[source] | Warmate: Training, HE-FRAG with 300g of TNT or HEAT (penetration 200–240mm of RHA ) Warmate 2: Training, HE-FRAG, thermobaric FAE or HEAT (penetration 400mm of RHA)[source] |
|---|
| Engine | Electric motor[source] | Electric motor[source] |
|---|
| Flight ceiling | >4,500 m (4.5 km) AMSL[source] | 9,800 ft (3,000 m) AMSL[source] |
|---|
| Flight altitude | >200 m (660 ft) AGL[source] | Warmate: 150–300 m (490–980 ft) AGL Warmate 2: 100–200 m (330–660 ft) AGL[source] |
|---|
| Accuracy | 2 m (6 ft 7 in) CEP[source] | 1.5 m (4 ft 11 in) CEP[source] |
|---|
| Unit cost | — | $26,459.93 in 2017 (equivalent to $34,754 in 2025)[source] |
|---|
| Propulsion | — | Electric motor[source] Electric motor[source] |
|---|
| Payload weight | — | 1.4 kilograms (3.1 lb)[source] |
|---|
| Cruise airspeed | — | 80 km/h (50 mph; 43 kn)[source] |
|---|
| Max horizontal speed | — | 120 km/h (75 mph; 65 kn)[source] |
|---|
| Max attack airspeed | — | 150 km/h (93 mph; 81 kn)[source] |
|---|
| Cruise altitude | — | 150 to 300 metres (500 to 1,000 ft) AGL[source] |
|---|
| CEP | — | 1.5m[source] |
|---|
| Operation ceiling | — | 500 m (1,600 ft)[source] |
|---|
| Reported operators |
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|---|
Range
Single source